2010-013A
The two main stages put the payload module on a suborbital trajectory; the final stage MIRV bus then performs the low-thrust orbit insertion burn, dragging the payload behind it into a 710 x 726 km x 92.0 deg orbit. The final stage ended up in a higher orbit of 716 x 1119 km.
| Cryosat | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2010 Apr 8 | 1357:04 | Launch by Dnepr | KB LC109/95 |
| T+1:50 Stage 1 sep | |||
| T+5:09 GO | |||
| T+5:54 St 2 sep | |||
| 1401 | T+5:55? DU on | ||
| 1412? | Plume shield sep | ||
| 1413 | T+16:28 Satellite separation | ||
| 1413? | DS MECO | ||
Payload:
- SIRAL SAR Ku-band interferometric radar altimeter 1 and 2
- DORIS receiver
- Laser retroreflectors
No comments:
Post a Comment